FIELD: weapons and ammunition.
SUBSTANCE: counterair missile comprises an engine, a warhead and a homing system with an approach angle sensor in the form of four sectors of light sensitive material. Behind each sector there is a resistive layer that has reduced resistance near radial edges of each sector in the sector zone of 5-15°. The counterair missile, with tail main or additional stabilisers separately or on a common race fixed by a fixture controlled in process of flight with a capability of discharge. The counterair missile has a wing with alternate sweep. The counterair missile has a removable wing or wings. The counterair missile for flight along a ballistic trajectory has a unit of meeting point calculation, a unit of travelling time calculation and a unit of ballistic trajectory calculation with account of engine traction.
EFFECT: increased efficiency.
8 cl, 16 dwg
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